Novel Mechanism of Instability Control using a Tapered Spike in Hypersonic Flow

Ashish Vashishtha, Shashank Khurana

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)
Original languageEnglish
Title of host publicationAIAA AVIATION 2021 FORUM
DOIs
Publication statusPublished - 02 Aug 2021

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